EP2387531A4 - Konfiguration eines steif bewehrten rotors - Google Patents
Konfiguration eines steif bewehrten rotorsInfo
- Publication number
- EP2387531A4 EP2387531A4 EP09838518.0A EP09838518A EP2387531A4 EP 2387531 A4 EP2387531 A4 EP 2387531A4 EP 09838518 A EP09838518 A EP 09838518A EP 2387531 A4 EP2387531 A4 EP 2387531A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- stiff
- rotor configuration
- plane rotor
- plane
- configuration
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/35—Rotors having elastomeric joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/33—Rotors having flexing arms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/37—Rotors having articulated joints
- B64C27/39—Rotors having articulated joints with individually articulated blades, i.e. with flapping or drag hinges
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C27/48—Root attachment to rotor head
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Tires In General (AREA)
- Discharge By Other Means (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP15192629.2A EP3034398B1 (de) | 2009-01-19 | 2009-01-19 | Konfiguration eines steifen rotors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US2009/031381 WO2010082936A1 (en) | 2009-01-19 | 2009-01-19 | Stiff-in-plane rotor configuration |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15192629.2A Division EP3034398B1 (de) | 2009-01-19 | 2009-01-19 | Konfiguration eines steifen rotors |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2387531A1 EP2387531A1 (de) | 2011-11-23 |
EP2387531A4 true EP2387531A4 (de) | 2014-11-12 |
EP2387531B1 EP2387531B1 (de) | 2015-11-04 |
Family
ID=42340026
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15192629.2A Active EP3034398B1 (de) | 2009-01-19 | 2009-01-19 | Konfiguration eines steifen rotors |
EP09838518.0A Active EP2387531B1 (de) | 2009-01-19 | 2009-01-19 | Konfiguration eines steifen rotors |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15192629.2A Active EP3034398B1 (de) | 2009-01-19 | 2009-01-19 | Konfiguration eines steifen rotors |
Country Status (5)
Country | Link |
---|---|
US (2) | US8956117B2 (de) |
EP (2) | EP3034398B1 (de) |
CN (1) | CN102317155B (de) |
CA (1) | CA2749118C (de) |
WO (1) | WO2010082936A1 (de) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3034398B1 (de) * | 2009-01-19 | 2016-12-07 | Bell Helicopter Textron Inc. | Konfiguration eines steifen rotors |
EP2457830B1 (de) * | 2010-11-25 | 2014-11-12 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Verbindung einer Rotorenschaufel zur Rotorennabe |
US9327832B2 (en) | 2011-10-03 | 2016-05-03 | Bell Helicopter Textron Inc. | Elastomeric bearing with tapered shims |
US10059438B2 (en) * | 2011-12-26 | 2018-08-28 | Textron Innovations Inc. | Hub assembly with grease lubricated roller bearing and tension-torsion strap |
EP2653384B1 (de) | 2012-04-18 | 2019-10-02 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Flügelbefestigung für einen lagerlosen rotor eines helikopters |
EP2653383B1 (de) | 2012-04-18 | 2016-04-13 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Rotorblatt eines lagerlosen Rotors eines Hubschraubers |
US9487291B2 (en) * | 2012-12-05 | 2016-11-08 | The Boeing Company | Apparatus, system, and method for pitching and twisting a blade of a rotorcraft |
US9457897B2 (en) * | 2013-02-27 | 2016-10-04 | Bell Helicopter Textron Inc. | Rotor system shear bearing |
US10336445B2 (en) | 2013-03-12 | 2019-07-02 | Bell Helicopter Textron Inc. | High flapping yoke hub assembly using a cylindrical elastomeric attachment to avoid holes |
US9505490B2 (en) | 2013-03-13 | 2016-11-29 | Bell Helicopter Textron Inc. | Composite rotor system using two race track style cantilevered yokes |
US9505489B2 (en) * | 2013-03-13 | 2016-11-29 | Bell Helicopter Textron Inc. | Flexing clevis arrangement bolted joint attachment for flexible rotor hub with high offset and high flapping |
US9656747B2 (en) * | 2013-03-14 | 2017-05-23 | Bell Helicopter Textron Inc. | Soft in-plane and stiff out-of-plane rotor system |
EP2818407B1 (de) * | 2013-06-24 | 2016-12-21 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Rotorsystem eines Hubschraubers |
US9499262B2 (en) | 2013-08-02 | 2016-11-22 | Bell Helicopter Textron Inc. | Composite flexure for tiltrotor rotor system |
US9334048B2 (en) | 2013-09-18 | 2016-05-10 | Bell Helicopter Textron Inc. | Elastomeric bearing having tapered layers |
US9657816B2 (en) * | 2013-11-01 | 2017-05-23 | Bell Helicopter Textron Inc. | Drive link for tiltrotor rotor system |
US9701403B2 (en) * | 2014-02-18 | 2017-07-11 | Bell Helicopter Textron Inc. | Broad goods composite yoke for rotor system |
US9873507B2 (en) * | 2014-02-26 | 2018-01-23 | Bell Helicopter Textron Inc. | Rotorcraft elastomeric bearing assembly |
FR3057541B1 (fr) | 2016-10-14 | 2019-03-29 | Airbus Helicopters | Amortisseur de trainee integre a l'interieur d'une pale d'un rotor |
US10994829B2 (en) * | 2017-09-22 | 2021-05-04 | The Boeing Company | Foldable rotor assembly for fixed-wing VTOL aircraft |
US11427315B2 (en) | 2019-06-26 | 2022-08-30 | Textron Innovations Inc. | Rotor blade control system |
KR20230147090A (ko) * | 2021-01-22 | 2023-10-20 | 오버에어, 인코퍼레이티드 | 전기 항공기를 위한 추진 시스템 |
CN117944869B (zh) * | 2024-03-27 | 2024-05-31 | 山西观复智能科技有限公司 | 一种半柔性三桨叶桨毂 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2351006A1 (fr) * | 1976-05-11 | 1977-12-09 | Westland Aircraft Ltd | Rotor pour helicoptere |
US20080003106A1 (en) * | 2005-09-30 | 2008-01-03 | The Boeing Company | Rotor apparatus and methods for vertical lift aircraft |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4462755A (en) * | 1981-08-24 | 1984-07-31 | The United States Of America As Represented By The Secretary Of The Navy | Anvil-strap rotor |
US4427304A (en) * | 1982-04-07 | 1984-01-24 | United Technologies Corporation | Method for cryogenic proof testing of rotating parts |
US4427340A (en) | 1982-06-24 | 1984-01-24 | Bell Helicopter Textron Inc. | Soft inplane bearingless helicopter rotor |
WO2003039950A2 (en) * | 2001-11-07 | 2003-05-15 | Rehco Llc | Propellers, propeller stabilizers, and propeller related vehicles |
US7665969B2 (en) | 2005-01-24 | 2010-02-23 | Bell Helicopter Textron Inc. | Assembly for providing flexure to blade system |
CN101583535B (zh) | 2006-01-13 | 2013-11-06 | 贝尔直升机泰克斯特龙公司 | 硬共面的、装有万向架的斜旋翼毂 |
EP3034398B1 (de) * | 2009-01-19 | 2016-12-07 | Bell Helicopter Textron Inc. | Konfiguration eines steifen rotors |
-
2009
- 2009-01-19 EP EP15192629.2A patent/EP3034398B1/de active Active
- 2009-01-19 WO PCT/US2009/031381 patent/WO2010082936A1/en active Application Filing
- 2009-01-19 US US13/144,448 patent/US8956117B2/en active Active
- 2009-01-19 CA CA2749118A patent/CA2749118C/en active Active
- 2009-01-19 EP EP09838518.0A patent/EP2387531B1/de active Active
- 2009-01-19 CN CN200980153945.4A patent/CN102317155B/zh active Active
-
2015
- 2015-02-17 US US14/623,615 patent/US9878782B2/en active Active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2351006A1 (fr) * | 1976-05-11 | 1977-12-09 | Westland Aircraft Ltd | Rotor pour helicoptere |
US20080003106A1 (en) * | 2005-09-30 | 2008-01-03 | The Boeing Company | Rotor apparatus and methods for vertical lift aircraft |
Non-Patent Citations (1)
Title |
---|
See also references of WO2010082936A1 * |
Also Published As
Publication number | Publication date |
---|---|
EP2387531B1 (de) | 2015-11-04 |
US9878782B2 (en) | 2018-01-30 |
US20110274548A1 (en) | 2011-11-10 |
CA2749118A1 (en) | 2010-07-22 |
US20150158583A1 (en) | 2015-06-11 |
CN102317155A (zh) | 2012-01-11 |
CN102317155B (zh) | 2014-08-06 |
EP3034398B1 (de) | 2016-12-07 |
EP2387531A1 (de) | 2011-11-23 |
US8956117B2 (en) | 2015-02-17 |
CA2749118C (en) | 2015-09-08 |
EP3034398A1 (de) | 2016-06-22 |
WO2010082936A1 (en) | 2010-07-22 |
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